holset hx50/52/55 service repair manual

Holset HX50/52/55Service Repair Manual

Copyright 2007, Cummins Turbo Technologies Ltd. All rights reserved.VGT, Command Valve and Super MWE are trade marks of Cummins Turbo Technologies Ltd.Holset and the Holset Logo are registered trade marks of Cummins Turbo Technologies Ltd.Cummins and the Cummins logo are registered trade marks of Cummins Inc.

Provided By: www.MyHolsetTurbo.com

HX50/52/55 Service Repair Manual Foreword

ForewordThis publication was written to assist with installation, maintenance and overhaul of the Holset HX50/52/55turbocharger. It is not a warranty of any kind expressed or implied.

The specifications and procedures in this manual are based on information in effect at the time of publication.Holset Service reserves the right to make any changes at any time without obligation. If differences are foundbetween your turbocharger and the information in this manual, contact your local Holset approved agent.

The latest technology and the highest quality standards are used in the manufacture of Holset Turbochargers.When replacement parts are needed, we recommend using only genuine Holset parts.

provided by: www.MyHolsetTurbo.com

HX50/52/55 Service Repair Manual Table of Contents

Table of Contents1: Introduction

About the Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:1

How to Use the Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:1

How to Order Holset Original Parts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:1

Description and Operation of Turbocharger . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:2

General Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:2

Introduction to Turbocharger Matching. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:2

Notes, Cautions and Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:3

Installation Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:4

Installation Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:5

Symbols . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1:6

2: Component Identification

Turbocharger Identification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2:1

Dataplate and CHRA (Core) of Turbocharger. . . . . . . . . . . . . . . . . . . . . . . . . 2:1

Installation Options . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2:2

Exploded Views . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2:3

Component List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2:6

Purchasable Service Tools . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2:7

3: Troubleshooting and DiagnosisFault Finding Chart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3:1

4: Component Testing and ReplacementService Tools . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4:1

On Engine Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4:2

Bearing Clearance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4:5

Turbine and Compressor Housings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4:6

Cleaning of Housings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4:13

5: Turbocharger Service and OverhaulService Tools . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5:1

Disassembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5:2

Component Cleaning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5:7

Inspection and Testing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5:9

Reassembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5:13

6: Service Data SheetsHX Range Service Data Sheets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6:1


http://www.holset.co.uk/partsservice/service/HX_Service_Data_Sheet.pdf

HX50/52/55 Service Repair Manual Introduction

1:1

About the ManualThe procedures in this manual were developed to instruct in the correct overhaul of the Holset HX50/52/55turbocharger for optimum performance and minimum maintenance operation.

How to Use the ManualThe manual is split into sections designed to provide service information in a logical sequence. The manualcontains links to help the user navigate between relevant sections. Users who are unfamilier with navigating inPDF documents are refered to Navigating in PDF documents in the Adobe® Acrobat® Reader™ help file.

Contents is an interactive page with links to all the sections. It can be accessed from any pagein the manual by clicking this icon.

Section 1 defines the layout of the manual, introduces the reader to the operation of the turbochargerand presents important installation guidelines.

Sections 2, 3 and 4 concentrate on Turbocharger Component Identification, Troubleshooting andDiagnosis, Component Testing and Replacement.

Section 5 identifies the Service and Overhaul procedures to be followed in the unlikley event of a major turbocharger malfunction.

Section 6 quantifies build data to ensure the turbocharger will continue to operate to Holset Servicestandard on completion of overhaul.

Manual sections 1 to 5 where applicable, appear as a self extracting compressed file which is organisedaccording to the steps needed to most easily and correctly maintain the operation of the turbocharger. Usersare required to download this file to hard disk. Section 6 has its own file identity and resides atwww.holset.co.uk. so that Holset can update the Service Data as changes occur. The links between manualand service data are active only when the user is connected to the Internet.

Chapter 6 has an expiry date to encourage users to discard outdated saved or printed versions and alwaysaccess the latest information available at www.holset.co.uk.

When using the manual on-line this icon will link to Holset’s website to help find your nearest agentfor advice and how to order Holset original parts.

How to Order Holset Original PartsTo make sure of optimum performance, certain items must be discarded during disassembly and replaced withnew for re-assembly. These items are indicated in the Service and Overhaul section with the use of a * symbol.All items showing a * are available in a basic overhaul kit.

To get the correct parts for your turbocharger, refer to the ‘component identification’ section of this manual tohelp you find the following information:

1) Refer to the exploded view and component list to define the major components to be replaced.2) Refer to the turbocharger’s dataplate which will be found on the compressor cover or wastegate

actuator to define the identifying information about your turbocharger build standard.3) Contact your local Holset agent with componant identification nos. and dataplate assembly no., serial

no. and turbocharger type.4) With this information, your local agent can provide you with the optimum kit of parts for re-assembling

your turbocharger for continued long life operation.



Description and Operation of Turbocharger

1:2

General InformationA turbocharger is a mechanical device which uses the engine’s exhaust gases to force more air into the enginecylinders. Hot exhaust gas energy is used to turn a turbine wheel and shaft. At the other end of the shaft is thecompressor impeller (or compressor wheel), which draws in air and forces it into the engine cylinders.

Supplying increased air mass flow to the engine provides improved engine performance, lower exhaust smokedensity, improved operating economy and altitude compensation. The turbocharger has proven to be one of themost beneficial devices for improving engine performance. It performs its job very well, as long as it is properlycared for.

Introduction to Turbocharger MatchingThe need for optimised matching over the engine speed rangeA standard turbocharger can be perfectly matched to only one particular engine condition, eg maximum torquespeed or maximum load speed. At this engine speed, the turbocharger supplies the optimum mass of air togive the required air/fuel ratio. At other speeds the air/fuel ratio cannot be held at the optimum hence fuelconsumption and emission levels worsen.

Engine emission legislations have forced manufacturers to improve their engine efficiencies, particularly at lowspeeds where low air/fuel ratios cause high smoke levels.

The Holset turbocharger is carefully matched to meet the required engine characteristics during applicationengineering. It is important that this match is maintained by using only Holset original turbine and compressorparts.

The importance of correctly servicing the turbochargerA turbocharger requires accurate assembly at point of manufacture. It is very important to adhere to settinglimits when servicing the turbocharger, as failure to do so could result in turbocharger or engine failure.

Effects of wrong matchPossible consequences if turbocharger boost pressure is too low:-

• Engine runs fuel rich • Fuel consumption increase

• Exhaust temperature increase • Smoke levels increase

• Hydrocarbon levels increase • Risks of failing emissions tests

• High cylinder temperature risks

damage to engine pistons

Possible consequences if turbocharger boost pressure is too high:-

• Engine runs fuel weak (lean) • Nitrous oxide levels increase

• Excessive boost overspeeds • Turbocharger bearing failure andturbocharger wheel fatigue problems

• Increased cylinder pressure risks damage • Intercooler load increases causing engineto engine head gasket, pistons and valves to overheat, risking piston damage


NoteHolset Service receives many turbocharger returns that are no fault found. Before assuming the turbocharger is not performing to specification always refer to the engine diagnostic system and the troubleshootingdiagnostic procedures of this manual.


1:3

Notes, Cautions and Warnings

Notes, Cautions and Warnings are used in this manual to emphasise important or critical instructions.

NoteInformation which is essential to highlight.

CautionMaintanence or Service procedures which if not strictly followed, will result in damage or destruction of the turbocharger.

WarningMaintanence or Service procedures which if not correctly followed will result in personal injury or loss of life.

WarningTurbocharger surface temperature during operation can achieve 700°C (1300°F). The HX50/52/55 turbocharger weighs up to 21.1 kg (46.5 lb) and is fitted with external parts that are sensitive to manual handling.

CautionThis turbocharger has been manufactured using piece part and rotor balance processes and MUST be check balanced on rebuild.If you intend to overhaul/repair a rotor balanced turbocharger, ensure that all the rotor parts have co-relation marks prior to disassembly so that they can be reassembled in the same relative positions.Balance limits for turbocharger rebuild are shown on Holset’s Service Data Sheet.It is important to note that operating a turbocharger with a rotor or core balance level greater than the published limits could cause turbocharger or engine failure. If you are in any doubt regarding the balancing process, please contact an approved Holset agent for assistance.

WarningSome parts are manufactured in Viton that requires special treatment in the case of repair and service after fire.

NoteHolset turbochargers can be remanufactured using recovered parts. Where it is necessary to dispose of components or whole turbochargers, an environmentally responsible process such as recycling should be used, with due regard to local laws.



Installation Data

1:4

1. Holset Service receives many turbocharger returns that are no fault found. Before assuming the turbocharger is not performing to specification always refer to the engine diagnostic system and the fault finding chart of this manual to make all the recommended health checks.

2. It is important that intake and exhaust systems are fitted in accordance with the recommendations of the Equipment and Engine manufacturers. Limiting mass inertia loading is critical to turbocharger wholelifeoperation. Maximum engine vibration input must not exceed 10g.

3. The air filter must remove particles greater than 5µm at an efficiency of 95% and be of sufficient capacity to match the air consumption of the engine. Recommended filters should always be used with a pressure drop indicator. Intake systems must be capable of withstanding depressions up to 6.9 kPa (1.0 lbf/in2).

4. Hose and clip connections of intake manifold systems must be capable of withstanding the turbocharger pressure ratio. V band clamps are preferred and must be used above 3:1 pressure ratio.

5. Exhaust systems must be capable of operating at exhaust back pressures of up to 10 kPa (1.5 lbf/in2).This limit is increased to 13.4 kPa (2.0 lbf/in2) if a catalytic converter is fitted. Exhaust brake applications are permitted to impose 450 kPa (65.3 lbf/in2) back pressure.

6. Oil should be filtered to 10µm with efficiency of 60% TWA (Time Weighted Average) /20 µm with efficiencyof 85% TWA. Efficiency assessed using ISO Standard 4572/SAE J 1858.

7. The oil quality must be as specified by the engine manufacturer and will be a minimum API SE - CD (MIL - L - 2104C) specification. Improved life can be obtained by using super high performance diesel (SHPD) oils, particularly in industrial applications which use extended oil drain periods.

8. Normal oil temperature is 95+/-5°C (203+/-9° F). It should not exceed 120°C (248°F) under any operating condition.

9. Any pre-lube oil must be clean and meet the minimum CD classification.

10. The orientation of turbine housing, bearing housing and compressor cover is fixed according to application. During installation, do not attempt to rotate these components. Inclined turbocharger installation is not recommended. If an installed angle is necessary, oil inlet centreline must be +/- 10 degrees from vertical and rotor centreline +/- 5 degrees from horizontal.

11. Holset permits oil return pipes to decline at an overall angle of not less than 30 degrees below horizontal.All turbocharger applications require a pipe of internal diameter greater than 19 mm which has integrated connectors. To ensure oil returns into the engine under all operating conditions, the return connection into the engine sump must not be submerged and the outlet flange of the turbocharger must be 50 mm above the maximum oil level of the engine sump pan. Crankcase pressure should be limited ideally to 0.8 kPa (0.12 lbf/in2) but 1.4 kPa (0.20 lbf/in2) can be accepted by reference to Holset.

12. Oil pressure of 150 kPa (20 lbf/in2) must show at the oil inlet within 3 - 4 seconds of engine firing to prevent damage to turbocharger bearing system. A flexible supply pipe is recommended.

13. The minimum oil pressure when the engine is on load must be 210 kPa (30 lbf/in2). Maximum permissible operating pressure is 400 kPa (58 lbf/in2) although 600 kPa (88 lbf/in2) is permitted during cold start up. Under idling conditions pressure should not fall below 70 kPa (10 lbf/in2).

14. Recommended oil flows for the turbochargers are 3 litre/min at idle and 3.5 - 4.5 litre/min above maximumtorque speed.

15. Do not use liquid gasket substances or thread sealant as any excess can enter the turbocharger oil system to obstruct flow.

16. Recommended coolant flows for the turbochargers are 3 litre/min at idle and 10 - 14 litre/min abovemaximum torque speed.

Note:

100 kPa = 1 bar (14.5037 lbf/in2 =psi).



Installation Checklist

1:5

1. Always understand why the original turbocharger needs replacing before fitting another unit.

2. Check the turbocharger dataplate to ensure the Part No. is correct for the engine/application.

3. Check the engine exhaust, intake and aftercooler systems are clean and without obstruction i.e. free from oil, gasket pieces, dust/dirt/carbon or foreign objects.

4. Replace the oil and air filters using replacement parts specified by the equipment manufacturer.

5. Change the engine oil using the type specified by the engine manufacturer.

6. Check that the turbocharger oil inlet and drain pipes and connectors are clean, free from obstruction and will not leak under pressure.

7. Check that the coolant pipes of water cooled bearing housing applications and connectors are clean, free from obstruction and will not leak under pressure.

8. To pre-lube the turbocharger bearings, pour some clean engine oil into the oil inlet and rotate the turbocharger rotor assembly by hand.

9. Check that the exhaust manifold flange is flat and undamaged. Mount the turbocharger on the flange and check that the turbine inlet gasket fits properly without obstructing the gas passages.

10. Assemble the air intake and boost outlet connections. Check that the connections are well made and will not leak in use.

11. Check the exhaust system is fitted using the original mounting arrangement provided by the equipment manufacturer. Always re-fit any supports/brackets back in position to ensure the system is correctly supported.

12. Assemble the exhaust system to the turbine housing outlet. Check that the gasket/connection is well made and will not leak in use.

13. Assemble any coolant pipes and check that the connections are well made, without obstruction and will not leak in use.

14. Assemble the turbocharger oil inlet pipe and check that the connection is clean, well made and will not leak in use.

15. Check all clamps and fasteners are correctly tightened to the torque recommended by the equipment manufacturer.

16. Make any ECU checks recommended by the engine manufacturer.

17. Crank the engine WITHOUT firing until engine oil flows out of the turbocharger drain flange.

18. Assemble the oil drain pipe and check that the connection is well made, without obstruction and will not leak in use.

19. Start the engine and run at idle speed for approximately 1 minute so that the oil supply system is fully operational.

20. Accelerate the engine and check that there are no leaks/obstructions of air/oil/coolant/gas under pressure.

21. Check that no hose or connection deforms under normal operation.

22. Before switching off the engine, leave it running at idle speed for at least 1 minute to cool the turbine.


Symbole - DeutschIn diesem Handbuch werden die folgenden Symbole verwendet, die wesentliche Funktionen hervorheben. DieSymbole haben folgende Bedeutung:

WARNUNG - Unterhaltungs und Wartungsverfahren müssen genau befolgt werden, da einNichtbeachten zu Personenschäden oder tödlichen Verletzungen führt.

ACHTUNG - Falls Unterhaltungs und Wartungsverfahren nicht genau beachtet werden, kann derTurbolader dadurch beschädigt oder zerstört werden.

AUSBAU bzw. ZERLEGEN.

EINBAU bzw. ZUSAMMENBAU.

INSRPEKTION erforderlich.

Teil oder Baugruppe REINIGEN.

DIMENSION - oder ZEITMESSUNG.

Teil oder Baugruppe ÖLEN.

WERKZEUGGRÖSSE wird angegeben.

ANZUG auf vorgeschriebenes Drehmoment erforderlich.

Sicherstellen, daß die AUSWUCHTMARKEN an der Rotor-Baugruppe richtig ausgerichtet sind.

Elektrische MESSUNG DURCHFÜRHREN.

Weitere Informationen an anderer Stelle bzw. in anderen Handbüchern.

Schutzkleidung muß immer getragen werden.

Deutet an, daß Teile schwer sein können.

Website-Verzeichnis mit Ihrem nächsten Holset-Händler.

Gehe zu Inhalt


Symbols

1:6

KG



1:7

Symbols - EnglishThe following group of symbols have been used in this manual to help communicate the intent of theinstructions. When one of the symbols appears, it conveys the meaning defined below.

WARNING - Serious personal injury or extensive property damage can result if the warninginstructions are not followed.

CAUTION - Minor personal injury can result or a part, an assembly or the engine can be damaged ifthe caution instructions are not followed.

Indicates a REMOVAL or DISASSEMBLY step.

Indicates an INSTALLATION or ASSEMBLY step.

INSPECTION is required.

CLEAN the part or assembly.

PERFORM a mechanical or time MEASUREMENT.

LUBRICATE the part or assembly.

Indicates that a WRENCH or TOOL SIZE will be given.

TIGHTEN to a specific torque.

Ensure that the BALANCE MARKS on the rotor assembly are in alignment

PERFORM an electrical MEASUREMENT.

Refer to another location in this manual or another publication for additional information.

Please wear protective clothing at all times.

Indicates components may be heavy.

Website access to find your nearest Holset Agent.

Go to contents

KG


Simbolos - EspañolLos simbolos siguientes son usados en estes manual para clarificar el proceso de las instrucciones. Cuadoaparece uno de estos simbolos, su significado se espcifica en la parte inferior.

ADVERTENCIA – Procedimientos de Mantenimiento o Servicio que al no seguirse resultarán endaños personales o pérdida de vida.

ATENCION – Procedimientos de Mantenimiento o Servicio que al no seguirse al pie de la letra,resultarán en el daño o la destrucción del turbosobrealimentador.

Indica un paso de REMOCION o DESMONTAJE.

Indica un paso de INSTALACION o MONTAJE.

Se requiere INSPECCION.

LIMPIESE la pieza o el montaje.

Ejecutese una MEDICION mec·nica o del tiempo.

LUBRIQUESE la pieza o el montaje.

Indica que se dar· una LLAVE DE TUERCAS o el TAMA—O DE HERRAMIENTA.

APRIETESE hasta un par torsor especifico.

Ceriórese de que est·n alineadas las marcas de balance en el rotor.

EJECUTESE una MEDICION eléctrica.

Para información adicional refiérase a otro emplazamiento de este manual o a otra publicaciónanterior.

Favor de siempre llevar ropa protectora.

Indica que los componentes pueden ser pesados.

Acceso a Sitio Web para localizar su agente Holset más cercano.

Ir a la tabla de materias


1:8

KG


Symboles - FrançaisLes symboles suivants sont utilisés dans ce manuel pour aider à communiquer le but des instructions. Quandl’un de ces symboles apparait, il évoque le sens défini ci-dessous:

ATTENTION DANGER - Procédures de maintenance ou d’entretien qui, si elles ne pas observéescorrectement, auront pour résultat des lésions corporelles ou un décès.

MISE EN GARDE - Procédures de maintenance ou d’entretien qui, si elles ne sont pas observéesstrictement, auront pour résultat de causer des dégâts au turbocompresseur ou de conduire à sadestruction.

Indique une opération de DEPOSE.

Indique une opération de MONTAGE.

L’INSPECTION est nécessaire.

NETTOYER la pièce ou l’ensemble.

EFFECTUER une MESURE mécanique ou de temps.

GRAISSER la pièce ou l’ensemble.

Indique qu’une DIMENSION DE CLE ou D’OUTIL sera donnée.

SERRER à un couple spécifique.

S’assurer que les repères d’équilibrage sur l’ensemble de rotor sont alignés.

EFFECTUER une MEASURE électrique.

Se reporter à un autre endroit dans ce manuel ou à une autre publication pour obtenir desinformation plus complètes.

Il faut toujours mettre vêtements de protection.

Indique que les composants peuvent être lourds.

Accès au site Web pour trouver l’agent Holset le plus proche.

Aller au sommaire


1:9

KG



1:10

Símbolos - PortuguêsOs símbolos a seguir serão utilizados neste manual para facilitar a comunicação das instruções e seuesignificados estão déscritos abaixo.

ATENÇÃO - Os procedimentos de Manutenção ou Serviços que não forem seguidos correctamenteresultarão em ferimentos pessoais ou riscos de vida.

AVISO - Os procedimentos de Manutenção ou Serviço que não forem rigorosamente seguidosresultarão em danos ou destruição do carregador turbo.

Indica um passe de DESMONTAGEM.

Indica um passo de MONTAGEM.

Requer inspeção.

LIMPE a peça ou conjunto.

Requer Medição mecãnica ou de tempo.

LUBRIFIQUE a peça ou o conjunto.

Indica necessidade de APERTO.

TORQUEAR de acordo com o especificado.

Assegure-se de que as MARCAS DE BALANCEAMENTO do conjunto eixorotor estejam alinhadas.

Requer medição ELÉTRICA.

Procure em outra seção deste manual ou em publicação par obter informações adicionais

Por favor, sempre utilize EPI (Equipamento de Protecao Individual)

Indica que os componentes podem estar pesados.

Visite o Website para encontrar o seu Agente Holset mais perto.

Vá para Conteúdo

KG


Turbocharger Identification

HX50/52/55 Service Repair Manual Component Identification

2:1

Dataplate

Center Housing Rotating Assembly (CHRA) (2)

35XXXXXPYYMMXXXXX

HX50/52/55NoteDataplates will be fitted to the compressor housing (8). The information from the dataplate must be quoted for service and parts support.



2:2

Installation Options

Type A HX50

Type B HX52

Type C HX55



Exploded View - HX50

2:3

34

22

5

88

57

6

1338

8

7

5154

61

41

59

6411

644

31

64

64

361211

33

1643

32

66

70

53

NoteExploded views represent a generic build standard. Parts may be added or subtracted in specific applications.



2:4


22

34

8

6229

61

7

66

33

1631

1236

11

64

43

32

3862

28

6

5

6411

4

64

64

70

53

13




2:5


22

34

8

6229

61

766

33

1631

1236

11

64

43

32

3862

28

6

5

6411

4

64

113

114

53

13


NoteOriginal models of HX55 featured clamp plate attachment of turbine housing.



Component List - HX50/52/55

2:6

Item No. Description Quantity

1 Repair Kit CHRA (core)* 1

2 CHRA (Core) 1

4 Bearing Housing 1

5 Turbine Housing 1

6 Assembly, Turbine Wheel 1

7 Compressor Wheel 1

8 Compressor Housing 1

11 Journal Bearing* 2

12 Thrust Bearing* 1

13 Split Ring Seal, Turbine* 1/2

16 Split Ring Seal, Compressor* 1

22 Retaining Ring, Inlet Baffle 1

28 V-band Clamp, Turbine 1

29 V-band Clamp, Compressor 1

31 Oil Slinger 1

32 O-Ring Seal, Bearing Housing* 1

33 Oil Baffle* 1

34 Inlet Baffle 1

36 Thrust Collar 1

38 Heat Shield 1

41 O-Ring Seal, Compressor Housing* 1

43 Oil Seal Plate 1

51 Clamp Plate, Compressor Housing 2

53 Gasket, Oil Outlet* 1

54 Lockwasher, Compressor Housing 8

57 Bolt, Turbine Housing 6

59 Bolt, Compressor Housing 8

61 Locknut, Compressor Wheel 1

62 Locknut, V-band* 2

64 Retaining Ring, Bearing (Snap Ring)* 4

66 Insert, Retaining Ring 1

70 Gasket, Oil Inlet* 1

88 Clamp Plate, Turbine Housing 3

105 Connector male, Water 2

113 Adapter, Oil Inlet 1

114 O-Ring Seal, Oil Inlet 1

115 O-Ring Seal, Water 2

NoteExploded views may not contain all listed components.



Purchaseable Service Tools

2:7

The following special tools can be purchased from your local Authorised Repair Location. The use of thesetools is recommended and where necessary they are shown in the appropriate service procedure.

Service Tools

Part No. Tool Description Tool Illustration

CautionAll Service and Maintenance settings are shown in Holset’s Service Data Sheet. It is essential that thesesettings are used. Common tools found in mechanic’s tool box not included.

4027204 E-Clip Tool

56662 Circlip Pliers



4027202 Wastegate Air Feed Adapter

4027203 Wastegate Air Feed Adapter



HX50/52/55 Service Repair Manual Troubleshooting and Diagnosis

Fault Finding chart

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Hig

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un

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g H

ot

Po

or T

ran

sien

t R

esp

on

se

Sm

oke

Cyc

lic S

ou

nd

fro

m t

he

Turb

och

arg

er

Oil

Lea

k fr

om

Co

mp

ress

or

Sea

l

Oil

Lea

k fr

om

Tu

rbin

e S

eal

Dirty air cleanerClean or replace element according to manufacturer s recommendations

Restricted compressor intake ductRemove restriction or replace damaged parts as required

Restricted air duct from compressor to intake manifoldRemove restriction or replace damaged parts as required

Restricted intake manifoldRefer to engine manufacturer s manual and remove restriction

Air leak in feed from air cleaner to compressorReplace seals, gaskets or tighten fasteners as required

Air leak in feed from compressor to intake manifoldReplace seals, gaskets or tighten fasteners as required

Air leak between intake manifold and engineRefer to engine manufacturer s manual and replace gaskets or tighten fasteners as required

Foreign object in exhaust manifold (from engine)Refer to engine manufacturer s manual and remove obstruction

Restricted exhaust systemRemove restriction or replace damaged parts as required

Exhaust manifold cracked, gaskets blown or missingRefer to engine manufacturer s manual and replace gaskets or damaged parts as required

Gas leak at turbine inlet/exhaust manifold jointReplace gasket or tighten fasteners as required

Gas leak in ducting after turbine outletRefer to engine manufacturer s manual and repair leak

Restricted turbocharger oil drain lineRemove restriction or replace damaged parts as required

Restricted engine crankcase breatherRefer to engine manufacturer s manual, clear restriction

Turbocharger bearing housing sludged or cokedChange engine oil and oil filter, overhaul or replace turbocharger as required

Fuel injection pump or fuel injectors incorrectly setRefer to engine manufacturer s manual and replace or adjust faulty components as required

Engine valve timing incorrectRefer to engine manufacturer s manual for correct settings and adjust as required

Worn engine piston rings or linersRefer to engine manufacturer s manual and repair as required

Burnt valves and/or pistonsRefer to engine manufacturer s manual and repair as required

Excessive dirt build up on compressor wheel and/or diffuser vanesClean in accordance with details in the appropriate Holset publication

Turbocharger damagedFind and correct cause of failure, repair or replace turbocharger as necessary

3:1


Dial Gauge and Dial Gauge Adaptor-0+

1010

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404050

MERCER

TYPE 20

HX50/52/55 Service Repair Manual Component Testing and Replacement

Service Tools

4:1

The following special tools are recommended to perform procedures in this manual. The use of these tools isshown in the appropriate procedure.


Torque Wrench



Oil LeakageAdapter M16 x 1.5

Flange fitting M8 x 1.25

Replacement gaskets, seals and adapters should befitted without sealant as this can contaminate the oil.Torque tighten adapter to value shown inService Data Sheet and flange fasteners to valuespecified by engine manufacturer.

It is important to avoid kinked pipes during servicingand subsequent operation.


On Engine Checks

4:2

Flange fitting M8 x 1.25

Replacement gaskets and flange fasteners should befitted without sealant as this can contaminate the oil.Torque tighten fasteners to value specified by enginemanufacturer.

All outlet pipes should be free flowing without kinks andsharp bends and decline at an overall angle not lessthan 30° below the horizontal.

Closed crankcase ventilation systems have a tendencyto deposit oil in the compressor housing. Wherepractical remove intake system pipework every50,000 km (30,000 miles) to check housing,compressor wheel and inlet baffle condition.

Always refer to Cleaning of Housings to cleanhousing. Rotor components can be cleaned using a nonmetallic bristle brush.

WarningThe oil inlet is pressurised and no service action should be taken with the engine running.

WarningOutlet oil is hot and no service action should be takenwith the engine running.

WarningAlways wear safety glasses during cleaning.



Gas LeakageTurbine housing flange leakage will cause sootformation on the flange. Check exhaust manifold toflange seal ensuring fastener torque meets enginemanufacturer’s recommendation.

Check flange for cracks.

Check Marmon and half Marmon connections (turbineoutlet to exhaust system) for fretting damage. Whereturbine housing damage is visible change housing.


4:3

Coolant LeakageHX50 - M16 x 1.5

HX55 - M18 x 1.5

Repair by replacement of coolant inlet and outletfittings. Where housing threads are damaged replaceturbocharger. Torque tighten adapters to value specifiedby engine manufacturerer.

Visual ChecksCheck for cracked, bent or damaged compressor wheelblades.

Where practical, check for cracked, bent or damagedturbine wheel blades.

CautionDo not use sealant as this may affect performance ofo-ring seals.

CautionNever attempt to straighten blades.



With intake system disconnected from compressorhousing, it may be possible to check visually for excessbearing axial and radial clearances.

If in doubt, the turbocharger must be removed fromengine to check bearing clearance againstrecommended values shown in Service Data Sheet.


KG

4:4

NoteSome turbochargers have a coating applied to the internal surface of the turbine housing. This special coating is abraded by the turbine wheel and may affect the bearing clearances until its unique form is fully formed.



Secure the turbine housing and check the axialclearance using a dial gauge.

Ensure clearance is within MIN/MAX values shown onService Data Sheet.

If axial clearance does not meet specification refer toturbocharger Service and Overhaul to strip and rebuildthe CHRA (core).


KG

Bearing Clearance

4:5

Check the radial movement at compressor impellernose using a dial gauge.

Ensure movement is within MIN/MAX TIR (TotalIndicator Reading) values shown onService Data Sheet.

If radial movement does not meet specification refer toturbocharger Service and Overhaul to strip and rebuildthe CHRA (core).

KG




Turbine HousingPlace turbine outlet on a clean flat surface. Mark turbinehousing, bearing housing and V-band clamp, turbine(where fitted). This action assists in the re-assemblyprocess defining correct component orientation.

KG


Turbine and Compressor Housings

4:6

V-band Option1/4 UNF 28 tpi (7/16 in)

Loosen locknut, V-band clamp (62) and discard.

KG

Clamp Plate OptionM8 x 1.25 (13 mm)

Secure turbine housing flange in vice.

Seized bolts may be freed by spraying with penetratingoil and soaking for twenty minutes or a period of timerecommended by the oil manufacturer.

Loosen and remove the six bolts and three clampplates.

KG

Using a soft hammer, tap turbine housing down againstsoft bench surface. As bearing housing and compressorhousing assembly comes loose gently lift it out ofturbine housing engagement

KG

CautionTake care not to shear the clamp plate bolts.

CautionTurbine blades can be damaged easily when the turbine housing is removed.


Cracking of the turbine housing inlet flange and inletduct generally requires turbine housing replacement.Acceptance and rejection guidelines are shown in theseillustrations. If an exhaust gasket is available, alwaysensure that any cracks lie within its sealing area.

Check turbine housing inlet flange flatness is within0.1 mm (0.004 in) before retaining component for re-use.


4:7

Flange Fasteners - Clearance HolesCheck fastener hole diameter is not more than 1.5 mmlarger than the max. thread diameter of the fastener.

Flange Fasteners - Threaded HolesM10 x 1.5

Check flange threaded holes with an M10 x 1.5 threadgauge.

No

Cra

cks

No

Cra

cks

Cracking of the internal wall at the entry to the turbinewheel (tongue) is an acceptable service condition andthe turbine housing may be re-used.

Always clean the turbine housing before re-assemblypaying particular attention to surfaces close to theturbine wheel and the bearing housing location. Refer toCleaning of Housings for details.

CautionTurbine housings can exhibit cracking when subject toexcessive thermal and mechanical loads.

CautionWhere a crack will cause leakage to atmosphere theturbine housing must be replaced.


To replace turbine housing position V-band clamp(where fitted) over the bearing housing and alignindelible ink marks applied during disassembly.

Apply anti seize compound to bearing housing locatingbore of the turbine housing.

Carefully slide bearing and compressor housingassembly into turbine housing. Use ink alignment markto locate housing assembly in correct orientation withthe turbine housing.


4:8


Place V-band clamp in correct orientation and torquetighten new locknut (62) to value specified in Service Data Sheet.



Install the three clamp plates and torque tighten the sixbolts to value specified in Service Data Sheet.

Depending on housing orientation, some clamp platebolts may have restricted access. In these cases, use asuitable torque wrench adapter attached to a speciallycalibrated torque wrench.

Ensure rotor assembly freely rotates.

CautionThe turbine blades can be easily damaged wheninstalling in the turbine housing

NoteSome turbochargers have a coating applied to the internal surface of the turbine housing. This special coating is abraded by the turbine wheel and may affect turbocharger rotation until its unique form is fullyformed.




Compressor HousingPlace turbine outlet on a clean flat surface. Markcompressor housing, bearing housing and V-bandclamp, compressor (where fitted) to record correctorientation. This action assists in housing orientationduring re-assembly.

KG


4:9


Loosen and remove the compressor end V-bandlocknut (62) and discard.

KG



Loosen and remove the 8 bolts, lockwashers and twoclamp plates.

KG

Use a soft hammer to gently tap the compressorhousing off the bearing housing.

CautionCompressor blades can be damaged easily when the compressor housing is removed.


The bearing housing to compressor housing joint isfitted with o-ring seal, compressor (41). This seal shouldbe removed and discarded at this stage.

The seal may be seated in the compressor housing orbearing housing dependent on the turbocharger model.


4:10

Inspect internal profile of compressor housing forscoring damage due to possible contact withcompressor wheel. Move to Cleaning of Housingsif deposits remain.

Replace with new if profile damage is visible.

CautionAlways fit a new seal on re-assembly.

Inlet baffle optionTo clean compressor housings fitted with an inlet baffleit is necessary to remove baffle.

Inlet baffle (A) is the old type; inlet baffle (B) is the newtype. Baffle (B) has been improved and no longerincorporates the four stepped areas. This gives the newbaffle increased service life.

Using a flat screw driver, carefully apply force in thearea shown (C) as the retaining ring starts to move,force the screwdriver under the ring as shown in (D).

A B

C D

CautionAlways fit the new type of baffle (B) on re-assembly.

CautionWhen removing the inlet baffle retaining ring, be careful not to damage the compressor wheel with the screw driver. Use a rag or rubber bung to protect the wheel.

WarningAlways wear safety glasses when removing or refitting retaining rings.


Push the screwdriver in an anti-clockwise (counter-clockwise) direction to force the retaining ring out of thegroove. Remove the retaining ring.

Remove the inlet baffle.


4:11

Following cleaning of the compressor housing, locate anew type of inlet baffle onto the location ledge of thecompressor housing inlet.

Hold one end of the retaining ring in position in itscompressor cover groove. Press the remainder of theretaining ring into position using free hand.

Use a flat screw driver to make sure the retaining ring iscorrectly seated in the compressor cover groove.

Place the turbine and bearing housing assembly on aclean surface. To refit compressor housing, lubricatenew o-ring seal (41) with clean engine oil and installinto retaining groove. Loosely fit V-band clamp (wherefitted). Carefully locate the compressor housing over thecompressor wheel.

CautionThe compressor wheel blades can be easily damagedwhen the CHRA is installed.







Install the two clamp plates and torque tighten the eightbolts to value specified in Service Data Sheet.


KG

4:12


KG


Place V-band clamp in position and torque tighten newlocknut (62) to value specified in Service Data Sheet.

KG





Visually inspect the parts to detect signs of burning andother conditions in order to obtain as much informationas possible before washing.


Cleaning of Housings

4:13

Soak the housings in a non-corrosive low flash pointmetal cleaner to loosen deposits.

Dry the components using compressed air.

Scale like deposits, if any, must be removed by using anon metallic bristle brush. After removing the deposits,re-wash and dry the components.

CautionHousing surfaces adjacent to turbine and compressor wheels must be clean, smooth and free from deposits.





It is permissible to bead blast the turbine housing ifchemical and brush cleaning is not effective.

After removing the deposits, re-wash and dry thecomponents.


4:14

WarningDo not bead blast Aluminium and Cast Iron components together.

CautionPrevent the bead spray impinging directly on clamp plate and turbine flange threads by masking or plugging



HX50/52/55 Service Repair Manual Turbocharger Service and Overhaul

Service Tools

5:1

The following special tools are recommended to perform procedures in this manual. The use of these tools isshown in the appropriate procedure. These tools can be purchased from your local Authorised Repair Location.


Torque Wrench

Dial Gauge and Dial Gauge Adaptor-0+

1010

2020

3030

404050

MERCER

TYPE 20






Disassembly

5:2

Locate the CHRA (2) on to a 19 mm 12 point socketlocated in a suitable fixture.

If no marks exist scribe the shaft and compressor wheelbefore removing the compressor wheel lock nut. Thewashing process may remove indelible ink so a filemark on the shaft and scribe line on the compressorwheel nose is recommended.

M8 L.H. (13mm)

Remove the locknut, compressor wheel (61).

Remove compressor wheel (7).

NoteLeft hand thread.

CautionAlways make sure the turbine wheel shaft and compressor wheel have alignment marks before disassembly of the CHRA.

NoteBefore disassembly, check for turbine and compressorblade damage. Measure bearing radial movement andaxial clearance to ensure the CHRA (core) is within the MIN/MAX values shown on Service Data Sheet.



Remove remaining CHRA from fixture and gently slidebearing housing (4) off the assembly turbine wheel (6).

It is permissible to tap the protruding turbine shaftgently with a soft hammer if the split ring seal/s arestuck in their bore.


5:3

Remove heat shield (38).

Carefully remove the split ring seal / seals, turbine (13) * and discard.

With bearing housing (4) on a flat clean surface, usecirclip pliers Part No 56662 to remove insert, retainingring (66).

It is practical to use free hand to contain disassembledring whilst releasing pliers.

CautionCare should be taken not to score the turbine wheel shaft assembly.

WarningAlways wear safety glasses when removing sealing rings.

WarningAlways wear safety glasses when removing retaining rings.


Remove oil seal plate (43) using mole (vice) grips.

If the oil seal plate is stuck in its location, it is permittedto use two screw drivers under the exposed lip to priseout seal plate.


5:4

Remove oil slinger (31).

Using piston ring expander pliers remove and discardsplit ring seal, compressor (16) * from oil slinger.

Remove and discard the o-ring seal, bearing housing(32) *.

WarningAlways wear safety glasses when removing sealing rings.


Remove oil baffle (33) * and discard.


5:5

Remove the thrust bearing (12) * from its pin locationsand discard.

Remove the thrust collar (36).

Using circlip pliers, Part No. 56664, remove the twocirclips (64*) and the journal bearing (11*) from thecompressor end and discard.



Turn the bearing housing over and repeat the processof bearing removal at turbine end.


5:6

Compressor Inlet Baffle (option)Where specified by the engine manufacturer, certainturbochargers can have a pressed steel baffle fitted intothe inlet section.

This item is not serviceable and if damaged, must bereplaced, as the geometry of the part is critical to theperformance of the baffle.

To clean compressor housings always remove inletbaffle.

Refer to Turbine and Compressor Housings forremoval instructions.




Visually inspect all parts to detect signs of burning andother fault conditions in order to obtain as muchinformation as possible before washing.


Component Cleaning

5:7

Soak the components in a non-corrosive low flash pointmetal cleaner to loosen deposits.

Dry the components using compressed air.

Protect the sliding surfaces of the cleaned parts againstcorrosion by applying clean engine oil.

M6 x 1.25

Scale like deposits, if any, must be removed by using anon metallic bristle brush. After loosening the depositswith the brush, wash and dry components as above.

Clamp plate threads can be cleaned using the specifiedthread tap.





Flange M10 x 1.5 - Clamp Plate M8 x 1.25

It is permissible to bead blast the turbine housing ifchemical and brush cleaning is not effective.


5:8

Oil fittings M16 X 1.5 - M8 x 1.25

Coolant fittings M18 x1.5 - M16 x 1.5

It is important that the oil chamber of the bearinghousing is free of carbon before re-building. If heavydeposits persist after repeat washing replace bearinghousing (4).

It is permissible to bead blast steel rotating parts.

WarningDo not bead blast Aluminium and Cast Iron components together.

CautionHousing surfaces adjacent to turbine and compressor wheels must be clean, smooth and free from deposits.Always protect threads during bead blasting andclean with the specified thread tap after blasting.

CautionDo not bead blast the bearing housing as this may damage critical bearing surfaces.

CautionBlasting specific areas for long periods of time may affect component balance. Protect thread of turbine wheel assembly.

CautionDo not bead blast the Aluminium compressor housing as this may damage critical surfaces.

CautionAlways clean components with compressed air after blasting.



Major ComponentsAssembly Turbine WheelPlace assembly, turbine wheel (6) on a vee block.Position a dial gauge on the turned surface of the shaftat the threaded end. Check dial gauge reading. Whereshaft bend is greater than the recommended maximumof 0.025 mm (0.001 in) replace the assembly.

-0+

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Inspection and Testing

5:9

Inspect split ring seal, turbine (13)* groove walls forwear. If groove width exceeds recommended maximumreplace assembly.

Single ring seal 1.69 mm (0.067 in)

HX50 dual ring seal 3.55 mm (0.140 in)

HX55 dual ring seal 3.30 mm (0.130 in)

If the wear step on the ring face exceeds 0.102 mm(0.004 in) replace split ring seal, turbine.

If the free gap of the ring is less than 2.0 mm (0.08 in)replace split ring seal, turbine.

Inspect the bearing journals for excessive scratchesand wear. Where scratching is excessive or whereeither journal diameter is less than the recommendedminimum of 12.19 mm (0.48 in) replace the assembly.

Inspect for cracked, bent or damaged blades.

Replace with new if any damage found.

CautionDo not attempt to straighten the turbine shaft.



Compressor WheelInspect compressor wheel (7), for cracked, bent ordamaged blades.

Replace with new if any damage found.


5:10

Compressor HousingInspect internal profile of compressor housing (8), forscoring damage due to possible contact withcompressor wheel.

Return to Component Cleaning if deposits remain.

Replace with new if profile damage is visible.

M6 x 1.25 (10mm)

Check clamp plate compressor housing threads. Ensureall threads are clean and use a thread gauge to checkthread condition.

Replace with new if thread damage will adversely affectclamp loading.

Turbine HousingClamp plates M8 x 1.25 (13 mm)Turbine housing flange M10 x 1.5

Inspect the turbine housing (5) profile for damagecaused by possible contact with the rotor. Inspect theouter and internal walls for cracks or flaking caused byoverheating. Check clamp plate threaded holes withthe specified thread gauge.

Check turbine housing inlet flange flatness is within0.1 mm (0.004 in). Check fastener hole diameter is notmore than 1.5 mm larger than the max. thread diameterof the fastener. Where studs have been removed checkflange threaded holes with the specified thread gauge.

Replace with new if any of the above features are noncompliant.

CautionDo not attempt to straighten blades.


Air and Liquid Cooled Bearing HousingsOil Flanges M8 x 1.25 - Oil Adapter M16 x 1.5

Inspect journal bearing bores for wear and score marks.Replace bearing housing (4) if a bore diameter exceedsa maximum of:

HX50 19.06 mm (0.75 in) - HX55 22.27 mm (0.877 in)

or when bore scratching is severe.

Ensure groove locations for retaining rings, bearing (64)are free from deposits and do not exceed width of:

HX50 1.07 mm (0.042 in) - HX55 1.25 mm (0.049 in)

Check that the oil cavity is free from carbon and anyentrained debris that may be the result of a failure.Ensure all oil port threads are clean then check with theappropriate thread guage.


5:11

Check oil seal plate, retaining ring groove does notexceed a maximum width dimension of:2 mm (0.079 in).

Small ComponentsOil SlingerInspect and replace oil slinger (31) if the piston ringgroove walls are scored or damaged or if groove widthexceeds a maximum of 1.68 mm (0.066 in).

Check for signs of rubbing and scoring on the thrustsurface and replace where damage is severe.

If the ring faces show any signs of wear replace thesplit ring seal, compressor (16).

If the free gap of the ring is less than 2.0 mm (0.08 in)replace the split ring seal, compressor (16) *.

CautionBearing housing clamp plate interface can corrode in high temperature operation. Bearing housings showing corrosion damage must be replaced.

Liquid Cooled Bearing HousingM16 x 1.5M18 x 1.5

Ensure all coolant port threads are clean then checkwith the appropriate thread gauge.


Heat ShieldCheck and replace if the heat shield (38) is distorted orif signs of rubbing or cracking are visible.


5:12

Thrust CollarCheck and replace if thrust collar (36) is scored onthrust face or if any cracks are visible.

Compressor Inlet Baffle OptionCheck baffle for debris entrainment damage. Always fitnew type inlet baffle on reassembly.

Refer to Turbine and Compressor Housings forre-fitting instructions.



Rotor Balance

A turbocharger should always have co-relation markson the end of the turbine shaft and impeller nose if ithas been disassembled according to the processdefined in Disassembly. The thrust collar and oilslinger will not have co-relation marks.


Reassembly

5:13

Components that should be included in rotor balanceare:

• Turbine wheel and shaft

• Thrust collar

• Oil slinger

• Compressor wheel

• Nut

Balance is achieved by relative rotation of componentsas indicated by the balance machine output.

The balance process requires a purpose built rig andcompliance with the rig procedure.

Rotor balance limits appear in the Service Data Sheet.

On achieving balance, parts should be permanentlymarked for subsequent re-alignment during reassembly.

Load Component

Rotate At Balancing Speed

CorrectiveAction Required?

Hold Steady Speed

Measure OutOf Balance

HaltRotation

CleanComponent

Display BalanceData

Take CorrectiveAction

Re-load Component

Unload Component

Unload Component

Balance Flow Chart

NO YES

CautionThis turbocharger may have been manufactured usingthe ‘separately piece part balanced’ process. Rotor balance MUST always be checked on re-build.

CautionOnly use genuine Holset compressor wheels and assembly turbine wheels which are individually check balanced for long life and quiet operation.

CautionAlways make sure the balance marks on the rotor assembly are in alignment when rebuilding the turbocharger.


Turbocharger Reassembly

Place bearing housing compressor mating face on aclean surface.

Fit inner turbine end retaining ring, bearing (64) * usingcirclip pliers Part No. 56664.


5:14

Lubricate the journal bearing (11) * with clean engineoil and install.

Fit the outer retaining ring (64) * with the bevelled edgefacing the bearing.

Turn the bearing housing over and repeat the retainingring (64) * and journal bearing (11) * installationprocess at compressor end.

Install heat shield (38).

WarningAlways wear safety glasses when refitting retaining rings.

CautionMake sure the circlips are always fitted with the bevelled edge facing the journal bearing. Premature failure will result from incorrect fitting.


Using expander pliers, install new split ring seal / seals,turbine (13) * to assembly turbine wheel (6). Someapplications contain dual ring seals. It is clear from thegroove width dimension whether single or dual split ringseals are required.


5:15

Lubricate the shaft with clean engine oil and insert intothe journal bearings. Positively locate the split ring seal/ seals (13) * into position and ensure the assemblyturbine wheel rotates freely.

Support the assembly turbine wheel (6) in a suitablefixture.

Ensure all thrust contact faces are clean.

Insert thrust collar.

Apply clean engine oil to installed thrust collar (36) andinsert thrust bearing (12) * on to its location pins.

WarningAlways wear safety glasses when refitting sealing rings.

CautionAlign dual split ring seals (13) so the gaps are positioned 180˚ apart. Gently press down on the turbine wheel. A slight rotation of the wheel will assist in properly locating the split ring seals.

CautionAlign the balance mark on the thrust collar with that on the shaft, if applicable.


Install the oil baffle (33) * into the oil seal plate (43).


5:16

Apply a small amount of engine oil to the o-ring andinsert the o-ring seal, bearing housing (32) *.

Install new split ring seal, compressor (13) * to oilslinger (31).

Install oil slinger (31) into oil seal plate (43).

WarningAlways wear safety glasses when refitting sealing rings.


Transfer assembly from fixture locating on turbine wheelnose to one locating on bearing housing.

Install oil seal plate (43) into the bearing housing (4).


5:17

Gently tap the oil seal plate (43) with a soft hammer toseat in position.

Locate part built CHRA on to 19 mm 12 point socket insuitable fixture or vice.

Use circlip pliers Part No. 56662 to install the insert,retaining ring (66). It may be necessary to lift thebearing housing to its upper clearance limit to fullyexpose circlip groove.

Use soft hammer and drift to ensure retaining ring (66)is properly located.

WarningAlways wear safety glasses when refitting retaining rings.

CautionDo not rest turbocharger on turbine wheel. Always usea suitable assembly fixture.

CautionThe retaining ring must be fitted with the chamfered face upwards away from the oil seal plate.

CautionAlign the balance mark on the oil slinger with that on the shaft, if applicable.

CautionVisually inspect to ensure that o-ring has not been cutduring oil seal plate insertion.


Install compressor wheel (7).


5:18

Brush the thread and nut face with an anti-seizecompound to avoid loss of alignment during torquetightening.

M8 LH (13 mm)

Install the locknut, compressor wheel (61) and tightento the torque value defined in the Service Data Sheet.

V-band OptionPlace turbine housing (5) on a clean surface. Place V-band clamp loosely into position on the turbine housing.Carefully slide CHRA (2) assembly into the turbinehousing.

CautionAlign the balance marks scribed on shaft and compressor wheel.

CautionEnsure that the balance marks remain aligned on compressor wheel and shaft throughout the torque tightening sequence.

NoteLeft hand thread.

CautionThe turbine wheel blades can be easily damaged when the CHRA is installed.



M6 (10 mm) 1/4UNF 28tpi (7/16 in)

Place V-band clamp, turbine (28) in position and torquetighten new locknut, V-band (62) * to value specified inService Data Sheet.



5:19



Locate the C.H.R.A. into the turbine housing (5).

Install the three clamp plates (88) and tighten the sixbolts (57) to the torque value specified in Service Data Sheet.

Depending on housing orientation, some clamp platebolts may have restricted access. In these cases, use asuitable torque wrench adapter attached to a speciallycalibrated torque wrench.

Check thrust clearance using a dial gauge. Ensureclearance is within MIN/MAX values shown onService Data Sheet.

-0+1010

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TYPE 20

Check compressor end radial movement using a dialgauge. Ensure clearance lies within MIN/MAX TIR (TotalIndicator Reading) values shown onService Data Sheet. -0+

1010

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50

ME

RC

ER T

YP

E 20






Place the turbine and bearing housing assembly onclean surface. To refit compressor housing lubricateo-ring seal with clean engine oil and install intoretaining groove. Loosely fit V-band clamp (wherefitted). Carefully locate the compressor housing over thecompressor wheel.


KG

5:20


Place V-band clamp, compressor (29) in position andtorque tighten new locknut (62) to value specified in Service Data Sheet.



Install the two clamp plates and torque tighten the eightbolts to value specified in Service Data Sheet.


KG

CautionThe compressor wheel blades can be easily damaged when the CHRA is installed.





Cummins Turbo Technologies Ltd.Aftermarket DivisionCroset AvenueHuddersfieldWest YorkshireHD1 6SEwww.holsetaftermarket.com

Copyright 2007, Cummins Turbo Technologies Ltd. All rights reserved.VGT, Command Valve and Super MWE are trade marks of Cummins Turbo Technologies Ltd.Holset and the Holset Logo are registered trade marks of Cummins Turbo Technologies Ltd.Cummins and the Cummins logo are registered trade marks of Cummins Inc.Part No. 4029550 Rev. 01 Ref. JV/KD Effect date 06.03

Holset HX50/52/55Service Repair Manual

holset hx50/52/55 service repair manual

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